Saturn Apollo Program
A J-2 engine undergoes static firing. The J-2, developed under the direction of the Marshall Space Flight Center, was propelled by liquid hydrogen and liquid oxygen. A single J-2 was utilized in the S-IVB stage (the second stage for the Saturn IB and third stage for the Saturn V) and in a cluster of five for the second stage (S-II) of the Saturn V. Initially rated at 200,000 pounds of thrust, the engine was later uprated in the Saturn V program to 230,000 pounds.
- Date
- 1960-01-01
- Collection
- MSFC
- Archive
- NASA Image and Video Library
- Type
- photograph
Public domainsafest
Reason: a NASA work: not copyrighted in the United States.
Read from: NASA media usage guidelines: NASA material is not copyrighted in the US unless noted; no third-party credit or mark found.
Credit line
"Saturn Apollo Program" (1960-01-01). NASA/MSFC. Public domain. https://images.nasa.gov/details/6975832Need photos for a whole script? Add Find Any Photo to Claude and ask for this one by its id: 83878.
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